Schweizer 1-35 NTSB Reports

 

 

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SGS 1-35 Safety Reports

The 1-35 has a great safety record.  Not one accident has been associated with an aircraft problem.  As usual, most have been pilot decision problems, or stall/spin in the pattern.

 

I post these for us all to learn from the experiences of others.

 

 

NTSB Identification: LAX83FA386 .

Accident occurred Sunday, August 14, 1983 at JAMUL, CA
Aircraft: SCHWEIZER SGS 1-35C, registration: N2941H (SN=91)
Injuries: 1 Fatal.

REPORTEDLY, AFTER WAITING ALMOST 2 HRS, THE PLT DECIDED HE WOULD FLY THE SAILPLANE, EITHER FOR 1 HR OR UNTIL THE OWNER ARRIVED, WHEN THE OWNER ARRIVED, HE OBSERVED THE SAILPLANE FLYING BACK & FORTH ALONG THE NORTH SIDE OF RIDGE AREA. SUBSEQUENTLY, THE ACFT CRASHED IN A WOODED AREA ON THE DOWNWIND SIDE OF A RIDGE THAT SLOPED DOWNWARD TO THE NORTH AT ABOUT A 30 DEG ANGLE. ATHOUGH THERE WERE NO KNOWN WITNESSES, THE OWNER SAW THE SAILPLANE DISAPPEAR BEHIND A RIDGE IN THE VICINITY OF THE ACCIDENT SIDE. DURING IMPACT, THE SAILPLANE STRUCK A TREE, APRX 12 FT TALL, & BROKE IT IN HALF. IT CAME TO REST ON TREES & BRUSH WITH EXTENSIVE DAMAGE TO THE NOSE & COCKPIT AREAS. NO PREIMPACT MALFUNCTION OR FAILURE OF THE SAILPLANE WAS FOUND. THE CRASH SITE WAS LOCATED IN AN AREA KNOWN TO HAVE PERIODS OF HIGH SINK. THE PLT WAS A NAVAL AVIATOR WITH ONLY ABOUT 3.4 HRS FLT TIME IN THIS MAKE & MODEL.

The National Transportation Safety Board determines the probable cause(s) of this accident was:

In-flight planning/decision ..Improper ..Pilot in command
Contributing Factors :

Weather condition ..Downdraft
Object ..Tree(s)
Lack of total experience in type of aircraft ..Pilot in command

NTSB Identification: NYC85FHM01
Accident occurred JUN-02-85 at MIDDLETOWN, NY
Aircraft: SCHWEIZER SGS-1-35, registration: N9JK   (SN=18)
Injuries: 1 Uninjured.

THE ACFT LANDED OFF THE ARPT AFTER THE PLT LOST ALT IN A SPIN. THE PLT WAS AFRAID THAT THE
GLIDER WOULD LAND SHORT IN TREES SO HE LANDED ON A HIGHWAY. THE HARD LNDG DAMAGED THE ACFT.

Probable Cause:

Airspeed..Improper..Pilot in command
Stall/spin..Inadvertent..Pilot in command

 

NTSB Identification: NYC86FA017 .

Accident occurred Friday, October 25, 1985 at NORTH CONWAY, NH
Aircraft: SCHWEIZER SGS-1-35C, registration: N2565H (SN=65)
Injuries: 1 Fatal.

DURING AN OFF AIRPORT LANDING ATTEMPT IN A CLEARED CORN FIELD, THE GLIDER WAS APPROACHING A TREELINE AT AN ALTITUDE OF 10 TO 20 FT AGL. WITNESSES OBSERVED THE GLIDER PULL UP AND BANK TO THE LEFT BEFORE FALLING NOSE FIRST INTO THE GROUND. THE PILOT'S LOG BOOK REFLECTED ONE FLIGHT IN THE PRECEEDING 12 MONTH PERIOD.

The National Transportation Safety Board determines the probable cause(s) of this accident was:

In-flight planning/decision ..Poor ..Pilot in command
Contributing Factors :Judgment ..Poor ..Pilot in command


NTSB Identification: LAX86LA316 .

Accident occurred Sunday, August 03, 1986 at MARANA, AZ
Aircraft: SCHWEIZER SGS-1-35, registration: N34180 (SN=20)
Injuries: 1 Uninjured.

A SCHWEIZER SGS 1-35, LANDED HARD AFTER A STEEP FINAL APPROACH. THE PILOT INDICATED THAT HE WAS HIGH ON FINAL APPROACH AND INITIALLY APPLIED 30 DEGREES OF FLAPS. HE WAS STILL TOO HIGH AND ELECTED TO USE 80 DEGREES (FULL) FLAPS. THE AIRCRAFT LANDED HARD NOSE DONW ON THE AIRCRAFT BELLY FORWARD OF LANDING GEAR. THE AIRCRAFT CANOPY WAS BROKEN IMMEDIATELY BY THE IMPACT. THE AIRCRAFT THEN OVERRAN THE DIRT RUNWAY AND CAME TO REST IN VEGETATION OFF THE END. THE PILOT ALSO INDICATED THAT THIS WAS HIS FIRST FLIGHT IN THIS MODEL GLIDER AND THAT THERE WERE NO MECHANICAL FAILURES OR MALFUNCTIONS WITH THE AIRCRAFT PRIOR TO THE ACCIDENT.

The National Transportation Safety Board determines the probable cause(s) of this accident was:

Level off ..Not performed ..Pilot in command
Planned approach ..Poor ..Pilot in command
Proper glidepath ..Not followed ..Pilot in command

Contributing Factors :

Lack of total experience in type of aircraft ..Pilot in command
Proper descent rate ..Exceeded ..Pilot in command
Lack of total experience in type of aircraft ..Pilot in command

 

NTSB Identification: LAX86FUG05 .

Accident occurred Saturday, September 27, 1986 at PALM SPRINGS, CA
Aircraft: SCHWEIZER SGS-1-35C, registration: N2673H (SN=73)
Injuries: 1 Serious.

DURING A PLEASURE FLIGHT, THE ACFT WAS NOT GETTING THE LIFT REQUIRED TO MAINTAIN ALT. THE PLT DECIDED TO RETURN TO THE ARPT, HOWEVER, ENROUTE THE PLT REALIZED THAT HE WOULD NOT MAKE IT BACK TO THE RWY. THE PLT DECIDED TO LAND IN AN EAST WEST DIRECTION ON A SANDY AREA AND DID NOT REALIZE UNTIL ON FINAL APPROACH THAT HE HAD A CONSIDERABLE CROSSWIND. ON SHORT FINAL THE NOSE OF THE ACFT RAISED, THE LEFT WING DROPPED AND THE ACFT ENTERED A SPIN. THE ACFT COLLIDED WITH THE TERRAIN IN A NOSE DOWN ATTITUDE.

The National Transportation Safety Board determines the probable cause(s) of this accident was:

Stall ..Uncontrolled ..Pilot in command

Contributing Factors

In-flight planning/decision ..Poor ..Pilot in command
Weather condition ..Unfavorable wind
Terrain condition ..Soft
Compensation for wind conditions ..Misjudged ..Pilot in command
Airspeed ..Not maintained ..Pilot in command
Remedial action ..Not performed ..Pilot in command

NTSB Identification: NYC89LA018 .

Accident occurred Sunday, October 09, 1988 at METHUEN, MA
Aircraft: SCHWEIZER 1-35C, registration: N2737H (SN=67?)
Injuries: 1 Minor.

THE PILOT REPORTED THAT HE FAILED TO CONNECT HIS AILERONS WHEN HE ASSEMBLED THE GLIDER. HE DID NOT MAKE A FLIGHT CONTROL CHECK AND ACCEPTED AN AERO TOW TO GET AIRBORNE. AFTER AIRBORNE, HE DISCOVERED THE MISTAKE AND STAYED ATTACHED UNTIL 1500 FEET AT WHICH TIME HE RELEASED. HE SAID TURBULENCE CAUSED THE GLIDER TO ENTER A SPIRAL AND WHEN HE RECOVERED, HE WAS TOO LOW TO MAKE A FIELD. HE SAID HE STRUCK A TREE ON APPROACH AND FLIPPED OVER.

The National Transportation Safety Board determines the probable cause(s) of this accident was:

PILOT UNCONTROLLED CONTACT WITH A TREE DURING A LANDING AFTER THE PILOT FAILED TO CONNECT HIS AILERON CONTROLS AND ACCEPTED A TOW TO GET AIRBORNE.

 

 

NTSB Identification: BFO90LA021 .

Accident occurred Sunday, November 12, 1989 at PAINT BANK, VA
Aircraft: SCHWEIZER SGS-1-35C, registration: N2880H (SN=70)
Injuries: 1 Uninjured.

ENROUTE THE PLT ELECTED TO RETURN TO HIS DEPARTURE ARPT DUE TO DETERIORATING LIFT CONDITIONS. CONDITIONS CONTINUED TO DETERIORATE AND THE PLT DIVERTED TO A CLOSER ARPT. HE REPORTED THAT TWO MOUNTAIN RIDGES HAD TO BE CROSSED TO REACH THE ARPT. HE WAS ABLE TO CROSS ONE RIDGE; HOWEVER, INSUFFICIENT LIFT REMAINED TO CLEAR THE SECOND RIDGE. THE PLT REPORTED THAT THERE WAS NO SUITABLE LANDING AREA AVAILABLE AND THE GLIDER WAS LANDED IN TREES.

The National Transportation Safety Board determines the probable cause(s) of this accident was:

THE PILOT'S IMPROPER INFLIGHT PLANNING WHICH LED TO AN OFF-AIRPORT LANDING AFTER ENCOUNTERING DETERIORATING LIFT CONDITIONS. CONTRIBUTING FACTORS WERE THE MOUNTAINOUS TERRAIN AND LACK OF A SUITABLE LANDING AREA.

 

 

NTSB Identification: NYC90LA193 .

Accident occurred Tuesday, August 14, 1990 at ERWINNA, PA
Aircraft: SCHWEIZER SGS 1-35, registration: N34461 (SN=41)
Injuries: 1 Minor.

DURING TAKEOFF ROLL THE TOW ROPE BECAME SLACK AND AS THE GLIDER STARTED ITS INITIAL CLIMB OUT TO ABOUT 50 FEET A.G.L. THE ROPE SLIPPED AFT OFF OF THE TOW HOOK. DURING THE OFF AIRPORT LANDING, THE NOSE TOUCHED A HIGH MOUND OF DIRT, DROPPING THE LEFT WING. THE PILOT LOST DIRECTIONAL CONTROL AND THE GLIDER SKIDDED ABOUT 40 FEET ON THE RIGHT WING COMING TO REST IN THE OPPOSITE DIRECTION OF LANDING.

The National Transportation Safety Board determines the probable cause(s) of this accident was:

INADVERTENT RELEASE OF THE TOW LINE AT LOW ALTITUDE. A CONTRIBUTING FACTOR WAS THE LANDING IN UNSUITABLE TERRAIN.

 

 

NTSB Identification: SEA92LA036 .

Accident occurred Sunday, January 05, 1992 at HOOD RIVER, OR
Aircraft: SCHWEIZER SGS-1-35C, registration: N2818H (SN=78)
Injuries: 1 Uninjured.

DURING THE TOW TO ALTITUDE, THE CANOPY FOGGED OVER. THE PILOT'S VISIBILITY WAS GREATLY REDUCED AND AFTER RELEASING AT 2,800 FEET, THE PILOT TRIED TO CLEAR THE CANOPY; HOWEVER, THE FLIGHT INADVERTENTLY ENTERED IMC. THE PILOT EJECTED THE CANOPY AND SPOTTED A FIELD. DURING THE LANDING ROLL, THE GLIDER COLLIDED WITH STUMPS AND CUT TREES.

The National Transportation Safety Board determines the probable cause(s) of this accident was:

POOR PREFLIGHT PLANNING AND PREPARATION ALONG WITH THE PILOT'S RESTRICTED VISIBILITY. FACTORS TO THE ACCIDENT WERE: CLOUDS AND VFR FLIGHT INTO IMC.

 

 

NTSB Identification: SEA92LA098 .

Accident occurred Wednesday, May 20, 1992 at BIG TIMBER, MT
Aircraft: SCHWEIZER SGS-1-35C, registration: N2739H (SN=69)
Injuries: 1 Uninjured.

DURING A CROSS COUNTRY FLIGHT, THE GLIDER WAS UNABLE TO MAINTAIN ALTITUDE DUE TO A LOSS OF LIFT. THE PILOT INITIATED A FORCED LANDING TO AN OPEN FIELD. WHEN APPROXIMATELY 30 FEET AGL, THE GLIDER ENTERED A HIGH SINK RATE. THE PILOT REDUCED THE ANGLE OF ATTACK AND RETRACTED THE FLAPS, HOWEVER, THE GLIDER CONTINUED TO SINK AND LANDED HARD.

The National Transportation Safety Board determines the probable cause(s) of this accident was:

AIRSPEED WAS NOT MAINTAINED. FACTORS TO THE ACCIDENT WERE: NO THERMAL LIFT AND INADEQUATE REMEDIAL ACTION.

 

NTSB Identification: LAX93LA324 .

Accident occurred Sunday, August 15, 1993 at WICKENBURG, AZ
Aircraft: SCHWEIZER 1-35C, registration: N2562H (SN=62)
Injuries: 1 Serious.

Several gliders were participating in an 80 mile round trip endurance competition and many of the pilots reported turning back early and landing at the gliderport, while others stated that they were forced to make off airport landings in the desert due to unfavorable conditions. The pilot noted that a good altitude margin was maintained during the flight outbound toward the goal until reaching an area about 12 miles west of Wickenburg. The pilot began to experience heavy sink and he decided to turn around and head for the Wickenburg airport. The pilot stated that his altitude continued to deteriorate to the point where the airport at Wickenburg was no longer reachable and an off airport landing in the desert was the only option. The pilot said he found a suitable landing area but had to maneuver on final approach to avoid a set of power lines. The pilot said that during the maneuver the glider stalled, entered a spin to the right and impacted nose first.

The National Transportation Safety Board determines the probable cause(s) of this accident was:

the pilot's failure to maintain an adequate airspeed margin while maneuvering to land, resulting in an inadvertent stall/spin.

 

FULL REPORT:

On August 15, 1993, at 1535 hours mountain standard time, a Schweizer 1-35C glider, N2562H, collided with the ground during an off airport forced landing in the desert near Wickenburg, Arizona. The glider, owned and operated by the pilot, was participating in an 80 mile round trip endurance competition at the time. Visual meteorological conditions prevailed and no flight plan was filed for the operation. The glider was destroyed in the ground collision sequence. The certificated commercial pilot, the sole occupant, sustained serious injuries. The flight originated at the Turf Soaring Gliderport in Paradise Valley, Arizona, on the day of the mishap at 1300 hours.

According to an FAA inspector from the Scottsdale, Arizona, Flight Standards District Office, several gliders were participating in the competition and the pilots reported that soaring conditions were not very favorable, with little lift available. Many of the pilots reported turning back early and landing at the gliderport, while others stated that they were forced to make off airport landings in the desert.

In his statement, the pilot noted that a good altitude margin was maintained during the flight outbound toward the goal until reaching an area about 12 miles west of Wickenburg. The pilot reported that he began to experience heavy sink and he decided to turn around and head for the Wickenburg airport. The pilot stated that his altitude continued to deteriorate to the point where the airport at Wickenburg was no longer reachable and an off airport landing in the desert was the only option. The pilot said he found a suitable landing area but had to maneuver on final approach to avoid a set of power lines. The pilot said that during the maneuver the glider stalled, entered a spin to the right and impacted nose first.

 

NTSB Identification: NYC97LA108 .

Accident occurred Sunday, June 08, 1997 at PEPPERELL, MA
Aircraft: Schweizer SGS 135, registration: N17976 (SN= 4)
Injuries: 1 Serious.

After 30 minutes of flying on a local flight, the pilot/owner of the glider entered a left traffic pattern for landing on runway 24 at the departure airport. The pilot determined that she was too high on final approach, and initiated a 360-degree turn to lose altitude. The pilot stated that during the turn to final, the left wing of the glider stalled. This induced a spin to the left at 300 feet, and the glider descended into a river. Winds at an airport 6 miles northeast were reported from 150 degrees at 10 knots.

The National Transportation Safety Board determines the probable cause(s) of this accident was:

The pilot's failure to maintain airspeed during a turn, which resulted in an inadvertent stall and subsequent uncontrolled descent into water.

 

FULL REPORT:

On June 8, 1997, about 1605 eastern daylight time, a Schweizer SGS 135, a glider, N17976, was substantially damaged during an uncontrolled descent into a river, while maneuvering on final approach to the Pepperell Airport (MA09), Pepperell, Massachusetts. The certificated private pilot sustained serious injuries. Visual meteorological conditions prevailed for the personal flight that originated at MA09, about 1530. No flight plan had been filed for the flight conducted under 14 CFR Part 91.

In the NTSB Form 6120.1/2, the pilot stated that she had intended to fly a local flight and return to MA09. After 30 minutes of flying, she entered a left traffic pattern for landing on runway 24, at MA09.

She further stated:

"...I was high on my turn to final, I assessed traffic, and proceeded to complete a 360 [degree] turn to lose excess altitude. As I turned onto final, the second time, the left wing of the glider stalled and induced a spin to the left from about 300 ft. AGL. The glider crashed into the Nashua River..."

The winds at an airport, 6 miles northeast of MA09, were reported from 150 degrees at 10 knots.

The pilot had accumulated 109 hours of total flying experience, of which 70 hours were as pilot in command, and 3 1/2 hours in make and model.

 

 

NTSB Identification: LAX98LA147 .

Accident occurred Tuesday, April 28, 1998 at MARICOPA, AZ
Aircraft: Schweizer SGS-1-35, registration: N34187 (SN=47)
Injuries: 1 Serious.

On April 28, 1998, at 1315 hours mountain standard time, a Schweizer SGS-1-35, N34187, crashed after premature release of the tow rope and impacted a ditch. The glider sustained substantial damage, and the pilot/owner, the sole occupant, suffered serious injuries. Visual meteorological conditions prevailed for the local personal flight and no flight plan was filed.

FULL REPORT:

On April 28, 1998, at 1315 hours mountain standard time, a Schweizer SGS-1-35, N34187, crashed after premature release of the tow rope and impacted a ditch. The glider sustained substantial damage, and the pilot/owner, the sole occupant, suffered serious injuries. Visual meteorological conditions prevailed for the local personal flight and no flight plan was filed.

In a written statement from the pilot towing the glider, he reported that the takeoff and initial climb were normal. About 450 feet agl, the glider pilot moved out of position to the right, which caused the tow plane to yaw hard to the left. After bringing the glider back to the normal tow position, the glider veered rapidly to the right. The tow plane yawed hard to the left and the towrope snapped while at an altitude of approximately 700 feet agl. The tow pilot reported that it is their usual practice to release the towrope at 2,000 feet agl. The tow pilot then returned to the airport for landing.

According to a Federal Aviation Administration (FAA) inspector from the Scottsdale, Arizona, Flight Standards District Office, witnesses reported that during takeoff they saw the glider veer to the right and saw the tow line break. As the glider pilot attempted to return to the airport to land, it impacted a ditch that ran between the two runways. Rescue workers reported that the pilot was incoherent and they suspected that he had suffered a stroke. One witness reported that the pilot had medical problems that prohibited him from flying more than 2 hours at a time. The pilot did not possess a medical certificate. FAA Regulation Part 61.103 states that a private pilot with a glider rating has only to "certify that he has no known medical defect that makes him unable to pilot a glider or free balloon, as appropriate."

The pilot spent approximately 1 month in the hospital for various injuries inflicted from the accident. His wife reported that he has no memory of the accident. She also reported that she was unable to find any aircraft or pilot logbooks. The pilot's family sold the glider and no further examination was possible.

 

 

NTSB Identification: SEA00LA085
Accident occurred: MAY-06-00 at SEASIDE, OR
Aircraft: Schweizer SGS 1-35, registration: N34173 (SN=12)
Injuries: 1 Uninjured.


This is preliminary information, subject to change, and may contain errors. Any errors in this report will be
corrected when the final report has been completed.

On May 6, 2000, approximately 1500 Pacific daylight time, a Schweizer SGS 1-35
glider, N34173, collided with trees during a forced landing about three miles east of Seaside, Oregon. The commercial pilot was not injured, but the aircraft, which was owned and operated by the pilot, sustained substantial damage. The 14 CFR Part 91 pleasure flight, which departed McMinnville Airport, McMinnville, Oregon, about four hours earlier, was being operated in visual meteorological conditions. No flight plan had been filed, and
there was no report of an ELT activation. According to the pilot, he had flown to an area near Astoria, Oregon, and then attempted to soar south along the western side of the Coastal Range. While passing southeast of Seaside, he entered an area of reduced lift, and elected to divert to the Seaside Airport. As he got closer to the airport, he entered an area of sinking air, and ultimately determined that he would not be able to safely reach
the airport. He therefore made a controlled forced landing in some young trees adjacent to a road running through the valley he was following toward Seaside.

 

FULL REPORT

On May 6, 2000, approximately 1500 Pacific daylight time, a Schweizer SGS 1-35 glider, N34173, collided with trees during a forced landing about three miles east of Seaside, Oregon. The commercial pilot, who was the sole occupant, was not injured, but the aircraft, which was owned and operated by the pilot, sustained substantial damage. The 14 CFR Part 91 pleasure flight, which departed McMinnville Airport, McMinnville, Oregon, about four hours earlier, was being operated in visual meteorological conditions. No flight plan had been filed, and there was no report of an ELT activation.

According to the pilot, he had flown to an area near Astoria, Oregon, and then attempted to soar south along the western side of the Coastal Range. He hoped to be able to fly south to Tillamook, and then cross back over the mountains and return to McMinnville. While proceeding south, he intended to land at Seaside, Manzanita, or Tillamook if he reached a point where it appeared he could not safely continue. Upon reaching an area about 10 miles southeast of Seaside, he elected to turn back to Seaside, as he felt that there was "no assurance" that he could safely continue on his planned route. Soon after turning toward Seaside, he entered an area of "strong sink" and the aircraft began to lose altitude rapidly. When he was about five miles from the airport, the pilot realized that he could not successfully reach Seaside unless he encountered an area of lift. Since there were no suitable landing-out areas in sight, the pilot continued toward the airport by following the Clark River Valley. When he reached a point approximately three miles east of Seaside, knowing that he could not continue much further, the pilot elected to make a controlled forced landing in some small deciduous trees adjacent to a road running through the valley he was following. Although the pilot was not injured, the aircraft sustained substantial damage when it collided with the trees.

 

 

NTSB Identification: NYC01LA225

Accident occurred Saturday, September 08, 2001 at Cumberland, MD
Aircraft:Schweizer SGS 1-35, registration: N2540H (SN=52)
Injuries: 1 Uninjured.

This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed.


On September 8, 2001, about 1620 eastern daylight time, a Schweizer SGS 1-35 glider, N2540H, was substantially damaged while landing at Greater Cumberland Regional Airport (CBE), Cumberland, Maryland. The certificated private pilot was not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the local personal flight conducted under 14 CFR Part 91. The flight had departed CBE about 1600.

The pilot reported that prior to the accident flight, he had not flown the make and model glider. He received a cockpit briefing from an instructor, and was then towed to 3,000 feet. He entered a downwind leg for runway 29 at 500 feet above the ground. The pilot added that his attention was diverted to another glider landing ahead of him, and the accident glider's spoil/flap combination was not as effective as other models he had flown. As a result, the glider was "high and fast". The glider touched down more than 1,800 feet beyond the approach end of the 2,442-foot long runway. It then bounced several times, and traveled off the end of the runway into a fence. The glider sustained damage to the wing spars and fuselage.

Examination of the wreckage by a Federal Aviation Administration inspector did not reveal any pre-impact mechanical malfunctions, nor did the pilot report any.

 

 

 

 

 

 

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